首页> 外国专利> Nozzles for combustors, combustors and gas turbines

Nozzles for combustors, combustors and gas turbines

机译:用于燃烧器,燃烧器和燃气轮机的喷嘴

摘要

A nozzle body 2 extending along the axis is provided, and the nozzle body 2 is formed along the axis Am, the first fuel passage 21 through which the first fuel F1 flows, and the first fuel A first fuel ejection path 22 extending toward the outer peripheral surface of the nozzle body as it faces toward the front end side from the passage 21 and ejecting the first fuel from the outer peripheral surface, and the radial direction of the axial line than the first fuel passage 21 It extends from the outside in the axial direction Da, and extends from the air flow path 24 toward the center of the tip of the nozzle body 2, and extends from the center of the tip of the air flow path 24 through which the purge air PA flows. A nozzle for a combustor having an air blowing path 25 for blowing purge air PA is provided.
机译:提供沿轴线延伸的喷嘴主体2,并且喷嘴主体2沿轴线形成,第一燃料F1流过,第一燃料F1流过,第一燃料通道21流过,第一燃料F1流通,并且第一燃料朝向外部延伸的第一燃料喷射路径22喷嘴主体的外围表面,当它面向从通道21朝向前端侧面朝向前端侧,并且从外周表面喷射第一燃料,并且轴向线的径向比第一燃料通道21从外部延伸轴向DA,并且从空气流动路径24朝向喷嘴主体2的尖端的中心延伸,并且从空气流路24的尖端的中心延伸,吹扫空气PA流过尖端。提供一种用于燃烧器的喷嘴,其具有用于吹风的吹扫空气PA的吹风路径25。

著录项

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号